2,679 research outputs found
Intertwining of simple characters in GL(n)
Let be a non-Archimedean local field and let be the general linear
group . Let , be simple characters
in . We show that intertwines with if and only if
is endo-equivalent to . We also show that any simple
character in is a -type.Comment: 7 page
Tame multiplicity and conductor for local Galois representations
Let be a non-Archimedean locally compact field of residual characteristic
. Let be an irreducible smooth representation of the absolute Weil
group \Cal W_F of and \sw(\sigma) the Swan exponent of . Assume
\sw(\sigma) \ge1. Let \Cal I_F be the inertia subgroup of \Cal W_F and
\Cal P_F the wild inertia subgroup. There is an essentially unique, finite,
cyclic group , of order prime to , so that \sigma(\Cal I_F) =
\sigma(\Cal P_F)\varSigma. In response to a query of Mark Reeder, we show that
the multiplicity in of any character of is bounded by
\sw(\sigma).Comment: Revised version with further detai
Langlands parameters for epipelagic representations of
Let be a non-Archimedean local field. An irreducible cuspidal
representation of is epipelagic if its Swan conductor
equals 1. We give a full and explicit description of the Langlands parameters
of such representations.Comment: 25 page
Cycles in the chamber homology of GL(3)
Let F be a nonarchimedean local field and let GL(N) = GL(N,F). We prove the
existence of parahoric types for GL(N). We construct representative cycles in
all the homology classes of the chamber homology of GL(3).Comment: 45 pages. v3: minor correction
Status of linear boundary-layer stability and the e to the nth method, with emphasis on swept-wing applications
The-state-of-the-art for the application of linear stability theory and the e to the nth power method for transition prediction and laminar flow control design are summarized, with analyses of previously published low disturbance, swept wing data presented. For any set of transition data with similar stream distrubance levels and spectra, the e to the nth power method for estimating the beginning of transition works reasonably well; however, the value of n can vary significantly, depending upon variations in disturbance field or receptivity. Where disturbance levels are high, the values of n are appreciably below the usual average value of 9 to 10 obtained for relatively low disturbance levels. It is recommended that the design of laminar flow control systems be based on conservative estimates of n and that, in considering the values of n obtained from different analytical approaches or investigations, the designer explore the various assumptions which entered into the analyses
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